Boeing 737-3B7

Service difficulty reports · 4,722

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7373B7'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SB05177Battery Pack · dischargedPIT - THE EMERGENCY LIGHTS WERE OUT IN THE FIRST CLASS SECTION AND FORWARD GALLEY. MAINTENANCE REPLACED THE BATTERY CELL ASSEMBLY IN THE FORWARD GALLEY. OPERATIONALLY CHECKS OK.Dec 28, 2005 · N516AU · Boeing 7373B7 · Emergency LightingSDR USAA051618Skin · crackedFOUUND FWD SERVICE DOOR-OUTER SKIN-UPPER HINGE CUT OUT. INSTALLED DOUBLER IAW TR 52-10-13, DEFECT SIZE: .25".Dec 21, 2005 · N517AU · Boeing 7373B7 · Service DoorsSDR USAA051617Skin · crackedFOUND FWD SERVICE DOOR-OUTER SKIN- LOWER HINGE CUT OUT. INSTALLED DOUBLER IAW TR 52-10-13, DEFECT SIZE: .25".Dec 21, 2005 · N517AU · Boeing 7373B7 · Service DoorsSDR USAA051591Skin · chafedUNDER DORSAL FIN, STA 860-887 S2L-S2R CHAFED. INSTALLED REPAIR DOUBLER, TRIPLER & FILLERS IAW EA 97215, SRM 53-60-01, EO 5304V147, DEFECT SIZE: 52 INCH LINEAR CHAFING, .018 INCH DEPTH MAX.Dec 20, 2005 · N530AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051590Skin · chafedSTA 860-887, S2L-S2R CHAFED. INSTALLED DOUBLER & RUB STRIPS IAW EA 97215, DEFECT SIZE: 52 INCH LONG, .018 INCH DEEP CHAFED AREA.Dec 20, 2005 · N530AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05171Sill · damagedENROUTE, THE FLIGHT LOST PRESSURIZATION AFTER REACHING CRUISE ALTITUDE. THE FLIGHT DESCENDED TO 10,000 FEET. THE OXYGEN MASKS DID NOT DEPLOY. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD OUTFLOW VALVE AS A PRECADec 15, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA200512006Skin · chafedFOUND 52 INCH LONG BY .018" DEEP CHAFED AREA AT STA 860-887 S2L - S2R. INSTALLED DOUBLER AND AND RIB STRIPS PER EA 97215.Dec 15, 2005 · N530AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05165Battery Pack · dischargedBDL - SEVERAL CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS OK.Dec 12, 2005 · N522AU · Boeing 7373B7 · Emergency LightingSDR USAA051504Skin · chafedFOUND STA 860-882 UNDER DORSAL FIN CHAFED. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-60-01, REPAIR 9 AND EA 97194, DEFECT SIZE:.Dec 12, 2005 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA200501496Skin · crackedPHX - DURING INSPECTION DISCOVERED FUSELAGE SKIN CRACK, 1.0 INCHES LONG, ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND 1.5 INCHES AFT OF BS 727D. MAINTENANCE TRIMMED OUT CRACK DAMAGE IAW BOEING 737-300 SRM 53-00-01 REPDec 11, 2005 · N328AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA200501480Light · inoperativeEEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT AT ROW 5, LT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Dec 3, 2005 · N328AW · Boeing 7373B7 · Emergency LightingSDR SB05159Sensor · out of adjustBOS - FLT203, AFTER TAKEOFF FROM BOS, CREW COULD NOT RETRACT THE LANDING GEAR. THE GEAR HANDLE WOULD NOT MOVE UP PAST THE OFF POSITION. FLIGHT RETURNED TO THE FIELD AT BOS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANDec 1, 2005 · N522AU · Boeing 7373B7 · Landing Gear Position and WarningSDR SB05155Controller · faultyFA REPORTED A LOUD SQUEAK AND VIBRATION FROM FIRST CLASS CABIN FLOORBOARDS. AT THAT TIME, THE CABIN PRESSURE BEGAN CLIMBING. CABIN ROSE TO APPROX 11,000 FEET. CREW INITIATED DESCENT TO 10,000 FEET AND PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES. CREW REPORTNov 24, 2005 · N517AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR SB05170Oxygen Mask · failedBNA FLT 53, EN ROUTE CLT TO MCI. DURING EMERGENCY DESCENT, MASKS DEPLOYED EXCEPT ROW 20. MAINTENANCE, REPLACED OXYGEN GENERATORS, REPACKED MASKS. FOUND MASK LANYARD CAUGHT AROUND DOOR LATCH ROW 20. REPOSITIONED, OPS GOOD.Nov 23, 2005 · N512AU · Boeing 7373B7 · Passenger Oxygen SystemSDR SB05152Outflow Valve · faultyCABIN PRESSURE CLIMBING, AUTO FAIL LIGHT ILLUM, EMERG DESCENT. PRESSURIZATION UNCONTROLLABLE, MASKS DEPLOYED EXCEPT ROW 20. FOUND LT SAFETY RELIEF VALVE FAILED. REPLACED LT & RT VALVE, FWD & AFT OUTFLOW VALVES, DELTA P MODULE, SELECTOR PANEL, PRESSURE CONTRNov 23, 2005 · N512AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR SB05169Oxygen Mask · failedCLT FLT 1058 DURING EMERGENCY DESCENT, CREW REPORTED THE OXYGEN MASKS AT SEAT 1DF, 3DF AND AT THE AFT LEFT LAV FLIGHT ATTENDANT STATION DID NOT DEPLOY. MAINTENANCE, DROPPED OXYGEN MASK DOORS, THAT DID NOT DEPLOY, REPLACED ALL AFFECTED OXYGEN GENERATORS AND RENov 22, 2005 · N512AU · Boeing 7373B7 · Passenger Oxygen SystemSDR SB05151Outflow Valve · faultyTHE AUTO PRESSURE CONTROL INOPERATIVE PER MEL 21-14A. AIRCRAFT LOST CABIN PRESSURE WITH OXYGEN MASKS DEPLOYING. CABIN WAS UNCONTROLLABLE IN ALL PRESSURIZATION MODES. DESCENDED TO 10,000 FT, CONTINUED TO CLT. LANDED, NO EMERGENCY DECLARED. CREW REPORTED OXNov 22, 2005 · N512AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR USAA051409Spar · crackedLBL 135.5, 12 INCHES FWD FROM REAR SPAR CRACKED. MAJOR REPAIR, REMOVED DAMAGE, INSTALLED REPAIR TEE, FILLERS, AND VERT STIFFENER IAW EA 97047. DEFECT SIZE: 1.5 INCH.Nov 22, 2005 · N525AU · Boeing 7373B7 · Wing SparSDR USAA200511006Skin · crackedA 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCH BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.Nov 15, 2005 · N373US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SAA200511006Skin · crackedA 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.Nov 15, 2005 · N373US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA200501422Circuit Board · faultyPHX - EMERGENCY LANDING - CREW REPORTED RT GREEN GEAR LIGHT REMAINED ON DURING ENTIRE FLIGHT, WITH GEAR UP. GEAR EXTENDED NORMALLY IN PHX. CREW DID MAKE A PRECAUTIONARY FLY BY THE TOWER PRIOR TO LANDING. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TNov 15, 2005 · N332AW · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA051377Angle · corrodedLEFT TRANSITION ANGLE, STA 727D-807 CORRODED. FABRICATED NEW TRANS ANGLE AND INSTALLED IAW SRM 53-60-53, SRM 51-10-02. DEFECT SIZE: .500 INCH AREA CORROSION AT EACH FASTENER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051378Floor Support · corrodedBS 500D BETWEEN 26L AND 26R CORRODED. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE IAW SRM 53-30-53 AND SRM 53-00-53. DEFECT SIZE: CORROSION AREAS APPROXIMATELY 1 INCH IN DIAMETER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051379Angle · corrodedTOP OF TRANSITION ANGLE BETWEEN STA 767 AND 787 CORRODED. REMOVED DAMAGED SECTION, FAB AND REPLACED WITH NEW SECTION IAW SRM 51-10-2 & BOEING DWG 65-47957. DEFECT SIZE: SPOTS OF CORROSION APPROXIMATELY .125 INCH IN DIAMETER.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051380Door Frame · crackedAFT CARGO DOOR FRAME AFT WEBBING CRACKED. FABRICATED AND INSTALLED NEW WEBBING IAW SRM 51-70-13. DEFECT SIZE: 1 INCH CRACK.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA051381Angle · corrodedRBL 13.80, STA 787-847 CORRODED. CUT OUT DAMAGED SECTION AND SPLICE IN NEW SECTION IAW SRM 53-00-53 FIG 201. DEFECT SIZE: 6 INCH CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051382Shear Tie · corrodedSTA 727E BETWEEN STRINGER 27L TO 27R CORRODED. INSTALLED REPAIR PARTS PER SRM 53-00-07. DEFECT SIZE: 2 INCH LONG AREA OF CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Internal Mounting StructureSDR USAA051383Support · corrodedSTA 294-312, LBL 12 CORRODED. REPLACE INTERCOSTAL MEMBER AND T-FITTING IAW SRM 51-10-02. DEFECT SIZE: INTERCOSTAL HAS A 70 INCH AREA OF CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051384Angle · crackedBS 294; S-17R; ATTACHED TO OUTBOARD SIDE OF ZEE ANGLE CRACKED. PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02. DEFECT SIZE: 1.5 INCH CRACK IN A 4 INCH LONG ANGLE.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051385Angle · corrodedBS 300-353; ZEE ANGLE AT S-17L CORRODED. REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE WITH NEW IAW SRM 51-10-02 BOEING DWG 65-17688. DEFECT SIZE: APPROX 1 X 43 INCH CORRODED AREA.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051386Angle · corrodedTRANSITION ANGLE 727B THRU 727D CORRODED. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-60-53, DEFECT SIZE: 1 INCH CORROSION.Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA051387Skin · crackedSTA 727D & 707E AT S-22L CRACKED. INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 201. DEFECT SIZE: TWO CRACKS MEASURING 1.45 INCH.Nov 15, 2005 · N512AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051389Stiffener · crackedAFT END OF LT PACK BAY AT I/B AFT CORNER CRACKED. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWG 65-45402. DEFECT SIZE: 1 INCH CRACK.Nov 15, 2005 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05145Charger · inoperativePIT - MAINTENANCE REPORTED THE AFT CABIN EMERGENCY LIGHTS FROM SEAT ROWS 17 THROUGH 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY AND CHARGER IN THE AFT CABIN. OPERATIONAL CHECK GOOD.Nov 14, 2005 · N395US · Boeing 7373B7 · Emergency LightingSDR USAA051366Angle · corrodedFOUND CORROSION BS 300-353 ZEE ANGLE AT S-17L. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE IAW 65-17688, DEFECT SIZE: 1 BY 43 INCHES.Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051365Angle · corrodedFOUND CORROSION ON R-1 DOOR THRESHOLD INNER CHORD ANGLE BS 296. REPAIR, DEFECTIVE PART REPLACED WITH IDENTICAL PARTY IAW SRM 51-10-02, DEFECT SIZE: 2" BY 5".Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051364Web · crackedFOUND CRACK FUSELAGE STATION 353 STRINGER 16 LEFT. REPAIR, CUT WEB TO REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-04, EA 97004 DEFECT SIZE: 2.1".Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA200511005Skin · crackedFOUND 3 INCH CRACK IN FUSELAGE SKIN AT STATION 727E AT STRINGER 23R.Nov 11, 2005 · N433US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA051363Intercostal · crackedSTA 344, STA 360, BL0 MAJOR REPAIR, FABRICATED NEW REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: .250".Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051362Frame · damagedFOUND HOLE IN FRAME STA 380, S15L. ENLARGED HOLE TO .125 AND INSTALLED RIVET IAW EA 97066, DEFECT SIZE: .100".Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA051355Attach Angle · crackedFOUND STR 25L AND FRAME AT BS 380 CRACKED. FABRICATED AND INSTALLED NEW ANGLE BOEING DWG 69-38780 AND SRM 53-00-01, DEFECT SIZE: 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051354Floorbeam · corrodedFOUND STA 344, LBL42-RBL31; AROUND CLIP NUT HOLES IN FLOOR BEAM CORRODED. REMOVED CORRODED OUT OF LIMITS SECTION OF "T" CAP FROM LBL31 TO RBL31 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051356Floorbeam · crackedFOUND BS28/LBL27 CRACKED. FABRICATED AND INSTALLED STIFFENER IAW SRM 51-10-02, DEFECT SIZE: 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051357Stringer Clip · crackedCRACK FOUND STATION 343 AT STRINGER 11R. STRINGER TIE CLIP WAS FABRICATED IAW BOEING DRAWING 69-38939-5, DEFECT SIZE: .025.Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA051359Floorbeam · corrodedFOUND STA 344, LBL 42-RBL3, AROUND CLIP NUT HOLES IN FLOORBEAM. REMOVED AND REPLACED T-CAP FROM LBL 1 TO RBL 32 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051360Intercostal · crackedFOUND CRACK BS312 BL0 CABIN FLOOR SUPPORT STRUCTURE. CUTOUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-11, DEFECT SIZE: .25".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051361Stiffener · crackedFOUND STA 328 LBL45 FWD ENTRY FLOOR SUPPORT STRUCTURE CRACKED. REPAIR, FABRICATED NEW L-ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWR 65-45812 DEFECT SIZE: .250"Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051358Floorbeam · corrodedFOUND CORROSION BS 328 AT RBL 15 AND 12. FABRICATED SPLICE ANGLES AND INSTALLED SPLICE ANGLES AND "T" CAP IAW SRM 53-10-51, DEFECT SIZE: 7" BY.65".Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA051352Angle · crackedFOUND STA 350 AT STRINGER 16L CRACKED. REMOVED, FAB, HEAT TREATED AND INST NEW ANGLE IAW SRM 51-10-02, DWG 69-26555 JOB CARD J020-37-20, DEFECT SIZE: .250" CRACK.Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA051351Channel · crackedFOUND BS 360; S15L CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED NEW CHANNEL IAW SRM 51-10-02, DEFECT SIZE: APPROX 1" CRACK.Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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